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www.sciencedirect.com Gamma-ray astronomy / Astronomie des rayons gamma – Vo The future of gamma-ray astronomy L’avenir de l’astronomie gamma Jürgen Knödlseder IRAP, 9, avenue du Colonel-Roche, 31028 Toulouse cedex 4, France Comptes Rendus Physique, Vol. 17, Issue 6, pp. 663-678 a r t i c l e Article history: Available online xxxx Keywords: i n f o a b s t r a c t The field of gamma-ray astronom decade. Thanks to the advent of (H.E.S.S., MAGIC, VERITAS) and th thousand gamma-ray sources ar Observing gamma rays photoelectric effect Compton scattering pair creation lenses pair convertors Cherenkov telescopes Compton telescopes coded masks Particle detectors space-based TeVPA2016(12-16September2016) ground-based 2 History of gamma-ray astronomy Number of detected sources in red 177 >3000 2010 HAWC Fermi INTEGRAL 32 2000 H.E.S.S. 271 COMPTEL 1980 MILAGRO B. Sripathi Acharya Early History The TIFR group started the field of ground-based -ray astronomy in India in 1969, soon after the announcement of the discovery of pulsars in 1968. Pulsars were proposed to be the site of origin of high energy cosmic rays and hence the sources of ultra high energy -rays. They searched for pulsed emission of -rays from 5 pulsars with the same periodicities as observed at radio frequencies [1]. 25 CGRO COS-B 1970 VERITAS The Cherenkov light was detected by 2 large search light mirrors ( f/0.45 mirrors of 90 cm dia) focused onto fast (56 AVP) photo-multipliers (PMT) placed at their foci. The full field of view of each mirror was . The approximate collection area of high energy -rays was and the threshold energy of detection . The mirrors, mounted on an orienting platform, tracked each pulsar for about an hour when it is close to meridian transit. Observations were made on clear nights in the years 1969 and 1970 at Mukurthi located at an altitude of 2.2 km above mean sea level in the Nilgiri Hills in South India. Not having found any significant flux of -rays from any source they placed upper limits on the flux of -rays of the order of [2]. Whipple 9 HEGRA …............. SMM 272 2. EGRET 1990 CELESTE MAGIC This activity was revived after a hiatus of 5 years with more number of mirrors and improved detection methods. For 10 years, an array of Cherenkov telescopes with a total mirror area of about was operated in and around Ooty (Now called Udhagamandalam) in southern India ( , , 2.3 km altitude). A photograph of the set-up is shown in figure 1. Later, this set-up was moved in the year 1986 to Pachmarhi ( , , 1075 m altitude) in the state of Madhya Pradesh, in central India, where the sky conditions for night sky observations are better than that at Ooty. A very systematic search for pulsed emission of -rays was made on a number of isolated pulsars [3] and X-ray binaries [4] using these set-ups at Ooty and.Pachmarhi. Crab, Vela, PSR0355+54, Geminga and Her X-1 showed positive signals on several occasions [5, 7, 6, 8, 9, 10, 11]. Thémistocle 2 HEAO 3 SAS 2 Ooty Figure 1. Compact array at Ooty 1960 balloons 1 Ranger 3 OSO 3 Explorer XI The BARC group started observing the night sky in the mid seventies at Gulmarg in Kashmir ( , , 2743 m altitude) using two bare faced PMTs (EMI 9545B) separated by 1 m and pointing up-wards in the sky (which may be likened to a wide angle telescope with a viewing angle of w.r.t. zenith) in the drift scan mode. In this mode the telescope is kept stationary, and the sky is scanned as Earth rotates. They reported [12] a non-random component in the arrival times of cosmic ray events for time separation of . Later following the TIFR group, they too installed [13] a similar set-up at Gulmarg, consisting of 6 equatorially mounted TeVPA2016(12-16September2016) Crimean AERE Harwell garbage bin Observatory 3 Nucleosynthesis in the Universe 2010 2000 2014: 56Co Achievements lines from SN Ia 2003: 60Fe lines from Galaxy 1994: 44Ti lines from Cas A 1990 1960 2013: Proton acceleration in SNR 2011: Crab nebula flares 2010: Fermi bubbles, First radio galaxy lobe, First nova 2009: First millisecond pulsars,! First starburst galaxies 1993: Galactic origin of cosmic rays 1992: Diffuse LMC emission 1973: GRB, solar deexcitation lines 1972: e+e- 511 keV line Cosmic accelerators 2009: First starburst galaxies 2008: Crab pulsar 2005: First binary 2004: First resolved SNR 2002: First unidentified TeV source 2000: First SNR 1992: Mkn 421 1989: Crab nebula 1988: 56Co lines from SN II 1984: 26Al line from Galaxy 1980 1970 Cosmic rays in the Galaxy and beyond 1981: 25 point-like sources 1978: First blazar 1974: Crab pulsar 1972: Diffuse Galactic emission 1969: Crab pulsar 1962: Cosmic background 1961: 22 photons > 50 MeV 1958: Solar flare TeVPA2016(12-16September2016) 4 Scientific Challenges The nature of Dark Matter • • • Indicates a major flaw in our understanding of nature Proposed solutions include new fundamental particles (WIMPs, axions, etc.) Decay products of these particles may be detectable in gamma rays TeVPA2016(12-16September2016) 5 Scientific Challenges The nature of Dark Matter • • • Indicates a major flaw in our understanding of nature Proposed solutions include new fundamental particles (WIMPs, axions, etc.) Decay products of these particles may be detectable in gamma rays The origin of Cosmic Rays • • • • Unveiling the Galactic PeVatrons Impact of low-energy cosmic rays on interstellar chemistry Cosmic-ray propagation Impact of environment TeVPA2016(12-16September2016) 6 Scientific Challenges The nature of Dark Matter The origin of Cosmic Rays The physics of Particle Acceleration • • • • Indicates a major flaw in our understanding of nature Proposed solutions include new fundamental particles (WIMPs, axions, etc.) Decay products of these particles may be detectable in gamma rays • • • • • • What mechanisms are actually at operation in a given source? Insights from variability ! (time domain astronomy) Elusive source classes Unveiling the Galactic PeVatrons Impact of low-energy cosmic rays on interstellar chemistry Cosmic-ray propagation Impact of environment TeVPA2016(12-16September2016) 7 JID:COMREN AID:3304 /SSU [m3G; v1.175; Prn:5/05/2016; 11:50] P.5 (1-16) J. Knödlseder / C. R. Physique ••• (••••) •••–••• 5 Space-based projects Table 1 Summary of instruments and mission concepts for space-based gamma-ray astronomy (see text). MDP indicates the minimum detectable polarization of an instrument. Detector technologies comprise time projection chambers (TPC), silicon trackers (Si), cesium iodide scintillators (CsI), scintillating fibers (fib.), lead tungstate scintillators (PbWO4 ), bismuth germanate scintillators (BGO), lutetium yttrium orthosilicate scintillators (LYSO), and magnetic spectrometers (B). Parameter AdEPT e-ASTROGAM Context Launch date Energy range (GeV) Ref. energy (GeV) !E/E A eff (cm2 ) Sensitivity (mCrab) Field of view (sr) Angular resolution MDP (10 mCrab) Technology R&D – 0.005–0.2 0.07 30% 500 10 t.b.d. 1◦ 10% TPC M5? 2029? 0.0003–3 0.1 30% 1500 10 2.5 1.5◦ 20% Si + CsI CALET ISS 2015 launched 0.02–10000 100 2% t.b.d. 1000 1.8 0.1◦ – fib. + PbWO4 DAMPE GAMMA-400 HARPO HERD PANGU China Russia ∼2021 0.1–3000 100 1% 5000 100 1.2 0.02◦ – Si + CsI R&D – 0.003–3 0.1 10% 2700 1 t.b.d. 0.4◦ t.b.d. TPC China >2020 0.1–10000 100 1% t.b.d. 10 t.b.d. 0.1◦ – Si + LYSO ESA/CAS? 2021? 0.01–5 1 30% 180 t.b.d. 2.2 0.2◦ t.b.d. Si (fib.) + B 2015 launched 2–10000 100 1.5% 3000 100 2.8 0.1◦ – Si + BGO • Detection sensitivities are still poor in the MeV domain • Considerable potential exists in using modern, pixelised semiconductor production interactions. This would lead to a system that space-proven is sensitive fromhighly the MeV to the GeV domain, going about more a compact configuration with a minimum of passive material detect gamma than detectors a factor 10in beyond predecessor instruments, opening up thisamount poorly explored energy band. to In addition, such a system rays through to Compton and pair interactions would be sensitive the polarization of creation incoming gamma rays, accessing a new physical dimension that provides invaluable information about the underlying emission processes and source geometries. energies, succeeding Fermi-LAT willwill be be challenging. The (Fermi Fermi-LAT tracker has a geometric area of 1.5 × • AtAthigher GeV energies, succeedingtoto Fermi-LAT challenging spacecraft weight is 4.3 tons, 2 1.5 m , the spacecraft a diameter of detector) 2.5 m, a height of 2.8 m and a mass of 4.3 tons, which is a very respectable satellite. difficult to buildhas a much bigger Making the much is bigger to increase the (i.e effective area wouldcan soon the maximum capacities of • Area oftelescope improvement angular resolution pointdetection spread function); be hit achieved by decreasing existing (and also planned) launch vehicles.spacing So the detection area cannotand be substantially density of tracker and increasing between tracker calorimeterexpanded. Significant improvement in sensitivity for pair-creation telescopes can only be achieved through a dramatic improvement in the angular resolution, especially at lower energies where the Fermi-LAT point spread function (PSF) exceeds several degrees. The best ways to • Potential to cover both aspects in a single mission improve the PSF are to decrease the density of the material in the tracker and to space the tracking element further apart [62]. This joins pretty much the needs expressed above for the low- to medium-energy domains, and both needs can be combined in a single mission providing a low-energy extension to Fermi-LAT. The following sections will describe some of the proposed instruments and mission concepts for the future study of the gamma-ray Universe from space. Table 1 provides a summary of the performance of the proposed instruments and mission TeVPA2016(12-16September2016) 8 concepts, as presented in the relevant references. The accuracy of the performance predictions varies between instruments and also depends on the maturity of the project, hence the table is only useful for order-of-magnitude comparisons. The Time Projection Chamber (TPC) 30cm)3 cubic TPC drift ee- Time Projection Chambers E Up to 5 bar. signal amplification and collection + e- e - 27 e AdEPT Micromegas + GEM gas amplification HARPO ollection on x, y strips, pitch 1 mm. FTER chip digitization, up to 50 MHz. cintillator / WLS / PMT based trigger micromegas + (1 or 2) GEM 5 3 10 102 Few MeV – GeV domain, polarimetry Pair conversion telescope Gas (Ar-based) filled TPC10(few bars pressure) V = 250V, E = 250V/cm V E V sect MCA E V = 250V, E = 250V/cm 400 250 270 50 5 5V 3 Target volume: 200 x 200 x 100 cm V = 250V, E = 250V/cm V = 250V, E = 750V/cm e-e+ pairs drift downwards to detector plane 10 µ ∝ A , A=2.08±0.05 Detectors • Gas electron multiplier and micro-well detector (AdEPT) 200 • 400Micro-mesh 600 800 1000 340 350 360detector 370 380 390 400 410 and microstrip V [V] charge [ADC] (HARPO) Prototypes built and tested Stratospheric balloon flights planned AdEPT proposed as MIDEX in U.S. COST 2014 12 mesh b trans b GEM drift 5 4 gem t gem t gem t gem t VGEM 20V Main peak, µM only Fe & cosmics caracterization 10 Main peak, µM+1GEM Escape peak, µM+1GEM 1 0 h. Gros, TIPP2014 rnard 10 4 • • • • • • total gain events/second IM A 695 (2012) 71, NIM A 718 (2013) 395 mesh Figure 2 - Schematic of the 3-DTI TPC technology showing how electron-positron pairs are tracked in 3-D. Components of the time projection chamber, micro-well detector plus GEM, and an avalanche in a single well are identitifed. HARPO • • • TeVPA2016(12-16September2016) 9 Time Projection Chambers Angular resolution improvement TeVPA2016(12-16September2016) Polarisation 10 e-ASTROGAM Sub MeV – GeV domain, polarimetry Compton and pair conversion telescope Detector • Double sided Silicon strip (DSSD) tracker • 3D imaging scintillator CsI(Tl) calorimeter ! read out by Si drift diodes • Plastic anticoincidence shield read out by SiPM Using technology heritage from existing satellites Proposed as ESA M5 mission Similar concept proposed as NASA MIDEX (ComPair) • • • e-ASTROGAM Measurement" • • • Pair event γ Silicon tracker Compton event γ Scintillator calorimeter θ Plastic anticoincidence system Track e+ e- TeVPA2016(12-16September2016) 11 Calor e-ASTROGAM hardware Payload" e-ASTROGAM Detail"of"the"detector-ASIC" bonding"in"the"AGILE"Si"Tracker" 8" • Tracker:"56"layers"of"4";mes"5×5"DSSDs"(5 600" in"total)"of"500"µm"thickness"and"240"µm"pitch" • DSSDs"bonded"strip"to"strip"to"form"5×5"ladders" • Light"and"s;ff"mechanical"structure" • Ultra"low-noise"front"end"electronics" " Sandwich panel PICSiT!CsI(Tl)!pixel!Design of the calorimeter composed of 1 module of • Calorimeter:"8 464"CsI(Tl)"bars"coupled"at"both" 14x14 modules of 64 crystals 64 crystals ends"to"low-noise"Silicon"Dria"Detectors" • ACD:"segmented"plas;c"scin;llators"coupled"to" SiPM"by"op;cal"fibers" • Heritage:"AGILE,"Fermi/LAT,"AMS-02,"INTEGRAL," Fermi/LAT"AC"system" LHC/ALICE…" " V.!Ta:scheff!for!the!e%ASTROGAM!Collabora:on!!! !!!!!!!!!!!!28th!Texas!Symposium! ! TeVPA2016(12-16September2016) ! !13 18!December!2015! 12 • Improve"angular"resolu;on"close" to"the"Compton"physical"limits" Simula;on" of" the" Cygnus" region" in" the" 1" " 3" MeV" energy" band" using"the"e-ASTROGAM"PSF,"from" an" extrapola;on" of" the" 3FGL" source"spectra"to"low"energies" Angular resolution (degree) potential Angular"resolu;on" e-ASTROGAM e -ASTROGAM science 6" 10 Fermi/LAT COMPTEL 1 Compton Pair e-ASTROGAM 10 -1 10 -1 1 10 10 2 10 3 10 4 Gamma-ray energy (MeV) V.!Ta:scheff!for!the!e%ASTROGAM!Collabora:on!!! !!!!!!!!!!!!28th!Texas!Symposium! ! TeVPA2016(12-16September2016) ! !13 18!December!2015! 13 Some other projects Pangu HERD Gamma-400 • • • • • • Fermi/LAT-like with increased spacing between tracker and calorimeter Better angular resolution Poorer sensitivity Status unclear • • • • Primarily a particle detector (like CALET, DAMPE) GeV (- TeV) domain 3-D cubic calorimeter surrounded by microstrip silicon trackers from five sides Weight limited to 2 tons (half of Fermi-LAT) Will be placed aboard Chinese space station (2020+) TeVPA2016(12-16September2016) • • • Few MeV – GeV domain, polarimetry Pair conversion telescope Tracker combined with magnetic spectrometer to fit into 60 kg payload allocation Submitted unsuccessfully to joint ESA/CAS small mission call 14 JID:COMREN AID:3304 /SSU [m3G; v1.175; Prn:5/05/2016; 11:50] P.10 (1-16) Ground-based projects J. Knödlseder / C. R. Physique ••• (••••) •••–••• 10 Table 2 Summary of future observatories and experiments for ground-based gamma-ray astronomy. Parameter CTA Site(s) Altitude (m) Latitude Start of operations Lifetime (years) Energy range (TeV) !E/E A eff (m2 ) Sensitivity (mCrab) Field of view Angular resolution t.b.d. ∼ 2000 t.b.d. 2020 30 0.02–300 10% 3 × 106 1 5◦ –10◦ 0.05◦ • • • • • • • HAWC Sierra Negra (Mexico) 4100 19◦ N started 2013 10 0.1–100 50% 30 000 50 1.8 sr 0.5◦ HiSCORE LHAASO MACE Tunka Valley (Russia) 675 51.8◦ N t.b.d. t.b.d. 50–10 000 10% 108 100 0.6 sr 0.1◦ Daocheng (China) 4300 29◦ N 2020? > 10 0.1–1000 20% 8 × 105 (KM2A) 106 (WCDA) 10 1.5 sr 0.3◦ Hanle (India) 4270 32.8◦ N 2016 t.b.d. t.b.d. t.b.d. t.b.d. t.b.d. 4◦ t.b.d. Imaging Air Cherenkov Telescopes (IACTs) have been proven most efficient to study gamma-ray induced atmospheric Cherenkov light (excellent angular resolution, strong background rejection power) Drawbacks are low duty cycles (~10%) and narrow fields of view (~5°) Performance increase through more telescopes covering a larger area and eventually using SiPM instead of PMTs Water Cherenkov Detectors (WCDs) are most successful devices for studying the tails of extended air showers (“tail catcher detectors”) While modest in angular resolution and background rejection, they have excellent duty cycles and wide field of view (complementary to IACTs) Performance increase through larger surface areas, moving the detector to higher altitude, and improving the detector configuration Open access observatories Fig. 3. Artists view of a CTA array site. TeVPA2016(12-16September2016) 15 Cherenkov Telescope Array Figure 2.3 – Artist impression of the southern CTA site, showing the array combining three different sizes of Cherenkov telescope, covering a multi-km2 area. The combination of a large number of telescopes of different sizes gives CTA tremendous flexibility of operation as well as unprecedented sensitivity and energy range. SST (!4m) questions. These three telescope sizes are referred to as the Large-Sized, Medium-Sized and SmallSized Telescopes (LSTs, MSTs and SSTs). The basic characteristics of these telescopes were fixed as requirements based on these early simulations, plus a first very large scale simulation of realistic CTA telescope arrays. Later large scale simulations served to assess the site-dependence of performance (in particular site altitude and geomagnetic field) and to establish appropriate telescope spacing. A final very large (200M HS06 CPU hours, 3 PB disk space) effort was used to perform a final fine-tuning of MST the layouts, which are presented in Figure 2.4. The chosen layouts may need to be adapted for ease of (!12m) deployment, analysis LST in particular for La Palma, which has more complex constraints. All simulation and tools used have been verified on operating Cherenkov telescope arrays and multiple independent chains (!23m) have been compared at all steps in the process. Paranal/Chile Type: La Palma La Palma/Spain (3AL4M15-5) Type: 23-m LST 23-m LST 12-m MST 12-m MST 4-m SST (MAGIC) North (x) is up West (y) is left North (x) is up West (y) is left 250 m 1000 m Circle: - 400 m Circles: - 400 m - 800 m - 1200 m 4 LSTs, 25 MSTs, 70 SSTs TeVPA2016(12-16September2016) 4 LSTs, 15 MSTs Figure 2.4 – Agreed layout of telescopes on the two sites in the southern hemisphere (left) and northern hemisphere (right). The southern site contains more telescopes and covers a larger area. The SST array has a large footprint to provide a very large gamma-ray collection, but with a relatively high energy threshold due to the smaller telescope size. The LSTs have 16 Cherenkov Telescope Array An Open Observatory 2. The CTA Observatory A world-wide endeavour Improvements everywhere Figure 2.1 –TeVPA2016(12-16September2016) Illustration of performance goals and associated science drivers. 2.2 Telescope Arrays 17 Large size telescopes Science drivers • • • Lowest energies (< 200 GeV) Transient phenomena DM, AGN, GRB, pulsars Characteristics • • • • • • • • • Parabolic design 23 m diameter 370 m2 effective mirror area 28 m focal length 1.5 m mirror facets 4.5° field of view 0.11° PMT pixels active mirror control Carbon-fibre arch structure (fast repointing) Array layout • • South site: 4 North site: 4 Status • • Some elements prototyped First full telescope under construction in ! La Palma (http://www.lst1.iac.es/webcams.html) TeVPA2016(12-16September2016) 18 Mid size telescopes Science drivers • • Mid energies (100 GeV – 10 TeV) DM, AGN, SNR, PWN, binaries,! starbursts, EBL, IGM Characteristics • • • • • • • Modified Davies-Cotton design 12 m diameter 90 m2 effective mirror area 1.2 m mirror facets 16 m focal length 8° field of view 0.18° PMT pixels Array layout • • South site: 25 North site: 15 Status • • Telescope prototyped (Berlin-Adlershof) Prototype cameras under construction (2 types: NectarCAM & FlashCam) TeVPA2016(12-16September2016) 19 Small size telescopes ASTRI SST 1M GCT Science drivers • • Highest energies (> 5 TeV) Galactic science, PeVatrons Array layout • • South site: 70 North site: - First CTA light Characteristics • • • • • • Davies-Cotton design 4 m diameter 8.5 m2 effective mirror area 5.6 m focal length 9° field of view 0.24° SiPM pixels Status • • Prototype telescope built Camera prototype under construction Characteristics Characteristics Status Status • • • • • • • • • Schwarzschild-Couder design 4.3 m primary diameter 1.8 m secondary diameter 6 m2 effective mirror area 2.2 m focal length 9.6° field of view 0.17° SiPM pixels • • • • • • • Schwarzschild-Couder design 4 m primary diameter 2 m secondary diameter 6 m2 effective mirror area 2.3 m focal length 8.6° field of view 0.16° SiPM pixels • Prototype telescope structure built Prototype telescope built • Tested with MAPMT-based CHEC camera Camera prototype under construction TeVPA2016(12-16September2016) 20 LHAASO – A multi component expe Some other projects HiSCORE LHAASO MACE Four 90000 m2 Water Cherenkov detectors. Each one has the size of HAWC • • • • Non-imaging air-shower Cherenkov light-front sampling Up to 100 km2 area covered Wide field of view (~0.6 sr) Extend sensitivity to the PeV regime Complemented by IACTs and surface & underground stations for measuring muon component of air showers 24 Wide FOV air Cherenkov image • Telescopes 400 burst detectors for high energy • • Hybrid detector array Gamma ray detectors • Large (4 x HAWC) Water Cherenkov detector array (0.1-30 TeV) • Electromagnetic particle detectors and muon detectors (30-1000 TeV) TeVPA2016(12-16September2016) • • 21 m diameter IACT to be installed at Hanle (4270 m a.s.l) Design inspired from H.E.S.S. II LHAASO 2 1 Km array 4300 m 21 Sensitivity: past – present – future JID:COMREN AID:3304 /SSU 14 [m3G; v1.175; Prn:5/05/2016; 11:50] P.14 (1-16) J. Knödlseder / C. R. Physique ••• (••••) •••–••• Fig. 5. Differential 5σ sensitivity of gamma-ray telescopes (1 erg cm−2 s−1 = 1 mW m−2 ). Future instruments are shown as solid lines, concepts based on TeVPA2016(12-16September2016) R&D work are shown as dashed-dotted lines and existing or past instruments are shown as dashed lines. Colors distinguish the energy22domains (blue for low and medium energy, green for high energy, red for very high energy and magenta for ultra high energy. The grey lines show the Crab differential energy flux, as well as 10%, 1% and 0.1% of that flux for reference. The lowest of the lines corresponds to a differential energy flux of 1 mCrab. The INTEGRAL JID:COMREN AID:3304 /SSU Conclusions [m3G; v1.175; Prn:5/05/2016; 11:50] P.14 (1-16) J. Knödlseder / C. R. Physique ••• (••••) •••–••• 14 Space-based • • Ground-based An instrument covering the MeV – GeV energy range has the highest discovery potential! (e.g. e-ASTROGAM, ComPair) Will enable • measurement of pion-bumps characteristic of hadronic accelerators in many sources • study of the still elusive low-energy cosmic-ray component • observation of gamma-ray lines (nucleosynthesis, de-excitation, ! e+e- annihilation) • gamma-ray polarisation measurements Fig. 5. Differential 5σ sensitivity of gamma-ray telescopes (1 erg cm−2 s−1 = 1 mW m−2 ). Future instruments are shown as solid lines, concepts based on R&D work are shown as dashed-dotted lines and existing or past instruments are shown as dashed lines. Colors distinguish the energy domains (blue for low and medium energy, green for high energy, red for very high energy and magenta for ultra high energy. The grey lines show the Crab differential energy flux, as well as 10%, 1% and 0.1% of that flux for reference. The lowest of the lines corresponds to a differential energy flux of 1 mCrab. The INTEGRAL sensitivity is for a typical observing time of 106 s [100]. The COMPTEL sensitivity is for the observing time accumulated during the whole duration of the CGRO mission (∼ 9 years). The AdEPT sensitivity is for a typical observing time of 106 s [63]. The e-ASTROGAM [66], HARPO [101], and Fermi-LAT [102] sensitivities are given after 3 years of scanning observations for a source at high Galactic latitudes [66]. The GAMMA-400 sensitivity is for a 30 days long observation of a source at high Galactic latitude [103]. The CALET, DAMPE and HERD sensitivities are for 1 year of observation time (adapted from [80]). The MAGIC stereo system [7], H.E.S.S., and CTA [104] sensitivities are for an effective exposure time of 50 hours. The ARGO-YBL sensitivity is after 6 years of observations [105]. The MILAGRO sensitivity is for 1 year of observations [90]. The HAWC sensitivity is after 5 years of observations [90]. The HiSCORE sensitivity is for a 100 km2 array after 5 years of survey observations, equivalent to an on-source exposure time of 1000 hours [92]. The LHAASO sensitivity is after 1 year of observations [106]. The Cherenkov Telescope Array will expand on all aspects of current IACTs (sensitivity, energy range, angular resolution) • Will enable • WIMP detections from few 100 GeV to few TeV and physics of the still elusive low-energy cosmic-ray component. e-ASTROGAM furthermore covers the MeV domain that is • linessearch of PeVatrons the nucleosynthesis entire Galaxy rich of gamma-ray which give access to nuclear cosmic-ray in excitations, processes, and the positron– electron annihilation features below ∼ 511 keV. The AdEPT and HARPO concepts are also promising in the medium- to • though measurement of gaseous sub-minute in toAGN high-energy domains, both employ large volume time projection variability chambers that still need demonstrate their compliance with a space environment. Stratospheric balloon flights, as planned for example for the AdEPT instrument, • comprehensive population studies of particle are here crucial to test the reliability of the instrument in a space-representative environment. Another important leap in sensitivity will be achieved in the very high energy domain by CTA, with a factor of ∼ 10 accelerators increase with respect to current telescopes. One of the key features of CTA will be the extended energy range from a few tens of GeV to above 100 TeV, which is nicely visible in Fig. 5. With a few 100 hours exposure time, CTA will reach milli• studies of particle acceleration in and particle Crab differential sensitivity, making it the most sensitive gamma-ray telescope ever. CTA will reach the expected gamma-ray emission from annihilation of WIMPs with massesnear in the few 100 GeV to few TeVsources domain, provided that their annihilation propagation individual cross section corresponds to the thermal relic density value. CTA will reveal thousands of very high energy gamma-ray • sources, enabling comprehensive population studies of particle accelerators in the Universe. For example, CTA will detect gamma-ray emission from young supernova remnants located at the opposite edge of the Galaxy, accessing thus the entire Galactic volume to search for the still elusive Galactic PeVatrons. For steady sources, CTA will surpass the Fermi-LAT sensitivity above ∼ 50 GeV. For short-time phenomena, such as gamma-ray bursts or gamma-ray flares, CTA will be several orders of magnitude more sensitive than Fermi-LAT even at lower energies, owing to its huge effective detection area of > 106 m2 (compared to ∼ 1 m2 for Fermi-LAT). CTA will thus open a new window for time-domain astronomy, probing for example sub-minute variability in active galactic nuclei. LHAASO will explore even higher energies than CTA, thanks to the KM2A detector that measures the muon content in TeVPA2016(12-16September2016) 2 23